Impact tests of a sphere and several cylinders of various masses and fineness ratios, all of aluminum, fired into an aluminum double-sheet structure at velocities near 7 km/sec, show that a cylinder, impacting in the direction of its axis, is considerably more effective as a penetrator than a sphere. Impacts of three cylinders of equal mass, but different fineness ratios, produced holes through the structures' rear sheet, whereas impact of a sphere of the same mass did not. Moreover, it was found that to prevent rear-sheet penetration, the mass of the 1/2-fineness-ratio cylinder had to be reduced by a factor greater than three. Further tests wherein the cylinder diameter was held constant while the cylinder length was systematically reduced...
With the growing threat of orbital debris impacts to space structures, the development of space shie...
The analysis of hypervelocity impact of particles on a detector in space, with flow and shock penetr...
The effectiveness of a meteoroid bumper in reducing meteoroid penetrations is discussed. The bumper ...
Results of a series of hypervelocity impact tests are presented. In these tests, 1.275-g, 9.53-mm-di...
This report describes the results of an investigation of phenomena associated with the oblique hyper...
The results of a continuing investigation of the phenomena associated with the oblique hypervelocity...
Small pyrex glass spheres, representative of stoney meteoroids, were fired into 2024-T3 aluminum alc...
Blunt hypervelocity projectile lift-drag ratio and impact velocity effects on target penetration and...
Small pyrex glass spheres, representative of stoney meteoroids, were fired into 2024-T3 aluminum alc...
All spacecraft confronts threat of space debris and meteoroids. Spherical projectiles are common sh...
All spacecraft confronts threat of space debris and meteoroids. Spherical projectiles are common sh...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
FSmall pyrex glass spheres were launched int aluminum double-sheet targets at velocities to 8.8 km/s...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
Dual-plate structure is very effective in the protection of space vehicle from hypervelocity im-pact...
With the growing threat of orbital debris impacts to space structures, the development of space shie...
The analysis of hypervelocity impact of particles on a detector in space, with flow and shock penetr...
The effectiveness of a meteoroid bumper in reducing meteoroid penetrations is discussed. The bumper ...
Results of a series of hypervelocity impact tests are presented. In these tests, 1.275-g, 9.53-mm-di...
This report describes the results of an investigation of phenomena associated with the oblique hyper...
The results of a continuing investigation of the phenomena associated with the oblique hypervelocity...
Small pyrex glass spheres, representative of stoney meteoroids, were fired into 2024-T3 aluminum alc...
Blunt hypervelocity projectile lift-drag ratio and impact velocity effects on target penetration and...
Small pyrex glass spheres, representative of stoney meteoroids, were fired into 2024-T3 aluminum alc...
All spacecraft confronts threat of space debris and meteoroids. Spherical projectiles are common sh...
All spacecraft confronts threat of space debris and meteoroids. Spherical projectiles are common sh...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
FSmall pyrex glass spheres were launched int aluminum double-sheet targets at velocities to 8.8 km/s...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
Dual-plate structure is very effective in the protection of space vehicle from hypervelocity im-pact...
With the growing threat of orbital debris impacts to space structures, the development of space shie...
The analysis of hypervelocity impact of particles on a detector in space, with flow and shock penetr...
The effectiveness of a meteoroid bumper in reducing meteoroid penetrations is discussed. The bumper ...